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Improvements to the Flight Analysis and Simulation Tool (FAST) and Initial Development of the Genesis Flight Mechanics Simulation for Ascent, Aerocapture, Entry, Descent, and Landing (A2EDL) Trajectory DesignThe NASA Engineering and Safety Center (NESC) was requested to provide significant enhancements to the Flight Analysis and Simulation Tool (FAST), a generic, variable-degree-of-freedom, multi-body ascent, aerocapture, entry, descent, and landing (A2EDL) flight simulation code and a key Agency analysis tool. This report details the upgrades to FAST that were completed, describes a change to the assessment’s scope that allowed its goals to be exceeded with a new and innovative approach, and discusses the results of the modified approach.
Document ID
20210014622
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Daniel G Murri
(Langley Research Center Hampton, Virginia, United States)
Daniel A Matz
(Johnson Space Center Houston, Texas, United States)
David A Hoffman
(Johnson Space Center Houston, Texas, United States)
Jon S Berndt
(Jacobs (United States) Dallas, Texas, United States)
Susan C Brown
(Jacobs (United States) Dallas, Texas, United States)
Lorraine E Prokop
(Johnson Space Center Houston, Texas, United States)
Date Acquired
April 27, 2021
Publication Date
April 27, 2021
Subject Category
Space Transportation And Safety
Report/Patent Number
NASA/TM-20210014622
NESC-RP-18-01309
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Professional Review
Keywords
NASA Engineering and Safety Center; Flight Analysis and Simulation Tool; Simulation; Flight Mechanics
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